The application discloses a kind of
landing gear inner tube surface scratch weak magnetic flaw evaluation method, its evaluation method includes the following steps: first need to carry out
surface cleaning pretreatment to
landing gear inner tube to be measured, and in the condition without additional excitation
magnetic field, using geomagnetic field as natural excitation source, geomagnetic field environment calibration is carried out to
landing gear inner tube surface, establishes background
magnetic field baseline, according to the outer
diameter size and surface curvature
radius R of landing gear inner tube.The application adopts flexible carrier to carry multiple sensors, and good adhesion of sensor and inner tube surface is realized by adaptive
layout mode, effectively overcome the influence of landing gear inner tube cylindrical surface curvature on detection
signal consistency, improve the
repeatability and reliability of detection, adopt the adaptive
noise suppression method based on
wavelet threshold, can retain weak scratch
magnetic leakage signal characteristics while effectively filtering geomagnetic
background noise and
circuit noise, compared with traditional filtering method has better
signal fidelity.